A parametric study of a gas-generator airturbo ramjet (ATR)-Reference-Cited by-同舟云学术

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A parametric study of a gas-generator airturbo ramjet (ATR)

Published:1986-06-16 Issue: Volume: Page:
ISSN:
Container-title:22nd Joint Propulsion Conference
language:
Short-container-title:

Author:

SNYDER CHRISTOPHER¹

Affiliation:

1. NASA, Lewis Research Center, Cleveland, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1986-1681

Reference14 articles.

1. ashington, D.C., 1985.

2. TABLE 111. CONDITIONS FOR FIGURES 2 TO 12 Altitude,a m (ft) . 30,480 (100,000) Sea level static airflow, kg/sec (lb/sec) . 22.7 (50) Compressor design eff1ciency.b percent . 85 Turbine efficiency,c percent . 80 Turbine inlet temperature,d K (OR) . 972 (1750) Gas-generator design pressure,e atm . 40

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